Method for producing a perforated nacelle inlet assembly

Patent metadata

Field	Value
Publication number	US-12448151-B2
Application number	US-202418775577-A
Country	US
Kind code	B2
Filing date	Jul 17, 2024
Priority date	Jul 15, 2022
Publication date	Oct 21, 2025
Grant date	Oct 21, 2025

Abstract

A perforation forming system includes a laser device and a control unit operably connected to the laser device. The control unit is configured to control the laser device to laser drill a plurality of perforations through a lipskin that has a curved contour. The lipskin includes a metallic coating that defines an exterior surface of the lipskin and a composite panel that defines an interior surface of the lipskin. The control unit is configured to form the perforations by controlling the laser device to emit laser beams that impinge upon the interior surface of the lipskin and penetrate the composite panel before penetrating the metallic coating.

First claim

What is claimed is:

1. A perforation forming system comprising:
a laser device;
a memory storage device that stores a set of instructions that are computer-readable; and
a control unit operably connected to the laser device and the memory storage device, wherein the control unit executes the set of instructions to control the laser device to laser drill a plurality of perforations through an entire thickness of a lipskin at different locations within a perforation zone of the lipskin so that a percent open area of the perforation zone is less than 2%, wherein the lipskin has a curved contour and includes a metallic coating that defines an exterior surface of the lipskin and a composite panel that defines an interior surface of the lipskin, wherein the laser device is controlled by the control unit to emit laser beams that impinge upon the interior surface of the lipskin and penetrate the composite panel before penetrating through the metallic coating.

2. The perforation forming system of claim 1 , further comprising a fume extractor device configured to extract gaseous byproducts from the air that are produced by the laser beams impinging on the lipskin.

3. The perforation forming system of claim 1 , further comprising a surface detector sensor mounted to the laser device and operably connected to the control unit, the surface detector sensor configured to generate sensor data indicative of a distance from a beam-emitting lens of the laser device to the interior surface of the lipskin.

4. The perforation forming system of claim 3 , wherein the control unit is configured to select or modify one or more parameters of the laser device based on the sensor data generated by the surface detector sensor.

5. The perforation forming system of claim 1 , wherein the laser device is a single fiber laser device.

6. The perforation forming system of claim 1 , wherein the control unit executes the set of instructions to control the laser device to emit the laser beams having a wavelength of about 532 nm.

7. The perforation forming system of claim 1 , wherein the perforation zone of the lipskin encompasses a leading edge of the lipskin.

8. The perforation forming system of claim 1 , wherein the control unit executes the set of instructions to control the laser device to laser drill the perforations so that the percent open area of the perforation zone is less than 1%.

9. The perforation forming system of claim 1 , wherein the control unit executes the set of instructions to control the laser device to laser drill the perforations to have an average entry diameter at the interior surface of less than 400 microns and an average exit diameter at the exterior surface of less than 100 microns.

10. The perforation forming system of claim 9 , wherein the control unit executes the set of instructions to control the laser device to laser drill the perforations so that the average entry diameter at the interior surface is less than 100 microns and the average exit diameter at the exterior surface is less than 60 microns.

11. The perforation forming system of claim 1 , wherein the composite panel includes a carbon fiber reinforced polymer (CFRP) material.

12. The perforation forming system of claim 1 , wherein the lipskin has an annular barrel shape and defines a central opening, and the laser device emits the laser beams from a location within the central opening of the lipskin.

13. The perforation forming system of claim 12 , further comprising an effector arm, wherein the laser device is mounted to the effector arm and the effector arm positions the laser device within the central opening of the lipskin.

14. The perforation forming system of claim 1 , further comprising a positioning platform configured to hold and rotate the lipskin while the laser device emits the laser beams that impinge on the lipskin.

15. The perforation forming system of claim 1 , wherein the control unit executes the set of instructions to control the laser device to laser drill the perforations so that a pitch between the perforations along the interior surface of the lipskin is no less than 0.5 mm and no greater than 1.5 mm.

16. A perforation forming system comprising:
a positioning platform configured to hold a lipskin that has an annular barrel shape and defines a central opening;
an effector arm;
a laser device mounted to the effector arm, wherein the effector arm is configured to position the laser device within the central opening of the lipskin;
a memory storage device that stores a set of instructions that are computer-readable; and
a control unit operably connected to the laser device and the memory storage device, wherein the control unit executes the set of instructions to control the laser device to laser drill a plurality of perforations through an entire thickness of the lipskin at different locations within a perforation zone of the lipskin so that a percent open area of the perforation zone is less than 2%, wherein the laser device is controlled by the control unit to emit laser beams that impinge upon an interior surface of the lipskin before penetrating through an exterior surface of the lipskin.

17. The perforation forming system of claim 16 , wherein the lipskin includes a metallic coating that defines the exterior surface of the lipskin and a composite panel that defines the interior surface of the lipskin, so that the laser beams impinge upon on the composite panel before penetrating through the metallic coating.

18. The perforation forming system of claim 16 , wherein the positioning platform is configured to rotate the lipskin.

19. The perforation forming system of claim 16 , wherein the laser device is a single fiber laser device, and the control unit executes the set of instructions to control the laser device to emit the laser beams having a wavelength of about 532 nm.

20. The perforation forming system of claim 16 , wherein the control unit executes the set of instructions to control the laser device to laser drill the perforations so that the percent open area of the perforation zone is less than 1%.

Assignees

• Boeing Co
• Cav Advanced Tech Ltd

Inventors

• Rust Charles William
• Weidler Iii John Alfred
• Wood Martin

Classifications

• B23K26/382

  by boring · CPC title

• B64D29/00

  Power-plant nacelles, fairings or cowlings · CPC title

• B64D15/06

  Liquid application · CPC title

• B23K26/0823

  Devices involving rotation of the workpiece · CPC title

• B23K2103/172

  wherein at least one of the layers is non-metallic · CPC title